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中文核心期刊

界面相和孔隙缺陷对平纹机织复合材料拉伸性能的影响机制研究

STUDY ON THE INFLUENCE MECHANISM OF INTERFACE PHASE AND PORE DEFECTS ON THE TENSILE PROPERTIES OF PLAIN WOVEN COMPOSITE MATERIALS

  • 摘要: 平纹机织复合材料在致密化过程中会因基体沉积不完美而导致出现孔隙缺陷, 同时界面相在平纹机织复合材料中起到传递载荷的作用. 因此, 建立考虑界面相和孔隙缺陷的平纹机织复合材料损伤本构模型, 以描述平纹机织复合材料在考虑界面相和孔隙缺陷影响下的力学行为, 对材料结构损伤容限设计与界面相材料选择十分重要. 以某平纹机织复合材料为研究对象, 在Hashin和最大应力损伤准则的基础上引入零厚度内聚力损伤模型和随机分布的孔隙缺陷, 模拟了其细观损伤起始及演化过程, 研究了其对平纹机织复合材料拉伸性能的影响机制, 发现界面相的引入会显著改变平纹机织复合材料的损伤分布, 使得原本平纹机织复合材料在径向拉伸载荷作用下的纤维束搭接处损伤为主变为单胞边缘处损伤为主; 孔隙率超过一定范围会改变平纹机织复合材料的损伤模式, 随着孔隙率的增大, 使得该平纹机织复合材料由纤维束、基体和界面相共同承力变为纤维束承力为主, 大大削弱了平纹机织复合材料的强度性能, 为其他机织复合材料强度性能的预测提供了一定的参考.

     

    Abstract: In the densification process of plain weave fabric composite materials, pore defects occur due to imperfect matrix deposition, and interfaces play a role in transmitting loads in plain weave fabric composite materials. Therefore, it is important to establish a damage constitutive model that considers the interface phase and pore defects to describe the mechanical behavior of the material under the influence of interface phase and pore defects, for the design of material structure damage tolerance and selection of interface phase materials. Taking a certain plain weave composite material as the research object, a zero-thickness cohesive damage model and random distributed pore defects were introduced based on the Hashin and maximum stress damage criterion, simulating the microscopic damage initiation and evolution process, and studying the influence mechanism of the plain weave composite material's tensile performance. The study revealed that the incorporation of an interface phase would significantly change the damage distribution of the composite material. When the plain weave composite materials are subjected to force, the interface phases induce cracks to occur at the edge of the model in the direction of the external load, preventing the cracks from directly extending through the fibers, thus changing the damage pattern from being mainly at the fiber bundle lap joints under radial tensile load to being mainly at the unit cell edges; when the porosity rate surpasses a specific range, it will lead to a significant alteration in the damage mode of the composites, and as the porosity rate increased, the material would change from being supported by the fiber bundle, matrix, and interface phase to being supported mainly by the fiber bundle, greatly weakening the material's strength performance. This research outcome provides certain reference basis for the prediction of the strength performance of other composites as well as the study on the influencing mechanism of tensile performance.

     

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